Referenced Items are not available for this document.
Many gun launched projectiles spin to maintain in-flight dynamic stability. This spinning often induces the gyroscopic phenomenon known as precession, or coning. Coning poses a problem for actively controlling the projectile. A control scheme is proposed that can compensate for the coning angle of the projectile and allow front-mounted canards to efficiently change the projectile flight path without reaching a stall condition. Closed-loop regulation and H2 control theories are employed to construct the controller.
Published in:
Control Applications (CCA), 2010 IEEE International Conference on
Date of Conference: 8-10 Sept. 2010
- Page(s):
- 1832 - 1837
- E-ISBN :
- 978-1-4244-5363-4
- Print ISBN:
- 978-1-4244-5362-7
- INSPEC Accession Number:
- 11624663
- Conference Location :
- Yokohama
- Digital Object Identifier :
- 10.1109/CCA.2010.5611245
- Product Type:
- Conference Publications
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